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2020-18-08: Engine Air Intake System

FAA order 2020-18-08 is an airworthiness directive in force since August 27, 2020. The FAA's subject line: Engine Air Intake System. It names Robinson R44: about 1,944 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Robinson Helicopter Company
Models
R44 II
On this site
Robinson R44 1,944 registered

Dates and paperwork

In force since
August 27, 2020
Published
August 27, 2020 (signed August 21, 2020)
Docket
FAA-2020-0786
Replaces
2019-12-18
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is superseding Airworthiness Directive (AD) 2019-12-18 for Robinson Helicopter Company (Robinson) Model R44 II helicopters. AD 2019-12-18 required inspecting certain engine air induction hoses (hoses) and replacing any hose that was not airworthy. AD 2019-12-18 also prohibited the installation of certain hoses. This AD continues to require inspecting those previously affected hoses and amends the applicability, clarifies an inspection requirement, adds a requirement to repeat the inspection, and expands the installation prohibition. This AD was prompted by an additional report of separation between the outer and inner hose layers. The FAA is issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (4,742 characters)
Adoption of the Amendment \n\n\n\tAccordingly, under the authority delegated to me by the Administrator, the FAA amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows: \n\nPART 39--AIRWORTHINESS DIRECTIVES \n\n0 1. The authority citation for part 39 continues to read as follows: \n\n\n\tAuthority: 49 U.S.C. 106(g), 40113, 44701. \n\n\n\nSec. 39.13 (Amended) \n\n0 2. The FAA amends Sec. 39.13 by: 0 a. Removing Airworthiness Directive (AD) 2019-12-18, Amendment 39-19673 (84 FR 32028, July 5, 2019); and 0 b. Adding the following new AD: \n\n\n\t2020-18-08 Robinson Helicopter Company: Amendment 39-21229; Docket No. FAA-2020-0786; Project Identifier AD-2020-00914-R. \n\n(a) Effective Date \n\n\n\tThis AD is effective August 27, 2020. \n\n(b) Affected ADs \n\n\n\tThis AD replaces AD 2019-12-18, Amendment 39-19673 (84 FR 32028, July 5, 2019) (''AD 2019-12-18''). \n\n(c) Applicability \n\n\n\tThis AD applies to Robinson Helicopter Company Model R44 II helicopters, certificated in any category, with an orange silicone engine air induction hose (hose) part number (P/N) A785-31 installed. This AD does not apply to helicopters with a black neoprene hose P/N A785-31 installed. \n\n(d) Subject \n\n\n\tJoint Aircraft System Component (JASC): 7160, Engine Air Intake System. \n\n(e) Unsafe Condition \n\n\n\tThis AD was prompted by reports of separation between the outer and inner layers of a hose. The FAA is issuing this AD to prevent blockage of air flow to the engine, engine stoppage, and subsequent loss of control of the helicopter. \n\n(f) Compliance \n\n\n\tComply with this AD within the compliance times specified, unless already done. \n\n(g) Required Actions \n\n\n\t(1) For helicopters with serial numbers (S/Ns) 14168 through 14314 inclusive (except S/Ns 14269, 14287, 14299, and 14304), or with an orange silicone hose P/N A785-31 installed after October 1, 2017, and before the effective date of this AD, within 10 hours time-in-service (TIS) after the effective date of this AD: \n\t(i) With the hose removed, inspect the inside of the hose for separation between the outer and inner layers, and flex the hose in all directions while listening for a crinkling sound, which is an indication of separation. \n\t(ii) If there is any separation or a crinkling sound, before further flight, remove the hose from service. \n\t(iii) If there is no separation and no crinkling sound, and the hose is marked with \n\n((Page 52893)) \n\ncode 3Q17 or 1Q18 or an illegible code, within 50 hours TIS, remove the hose from service. \n\t(2) For all helicopters identified in paragraph (c) of this AD, accomplish the inspection required by paragraph (g)(1)(i) of this AD within 100 hours TIS after the effective date of this AD or at the next annual inspection after the effective date of this AD, whichever occurs first, and thereafter at intervals not to exceed 100 hours TIS or at each annual inspection, whichever occurs first. If there is any separation or a crinkling sound, before further flight, remove the hose from service. \n\t(3) As of July 5, 2019 (the effective date of AD 2019-12-18), do not install on any helicopter an orange silicone hose P/N A785-31 marked with code 1Q18. \n\t(4) As of the effective date of this AD, do not install on any helicopter an orange silicone hose P/N A785-31 marked with code 3Q17 or an illegible code. \n\n(h) Alternative Methods of Compliance (AMOCs) \n\n\n\t(1) The Manager, Los Angeles ACO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the certification office, send it to the attention of the person identified in paragraph (i) of this AD. Information may be emailed to: [email protected]. \n\t(2) Before using any approved AMOC, notify your appropriateprincipal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. \n\t(3) AMOCs approved for AD 2019-12-18 are approved as AMOCs for the corresponding provisions of this AD. \n\n(i) Related Information \n\n\n\tFor more information about this AD, contact Roger Gretler, Aerospace Engineer, Los Angeles ACO Branch, Compliance & Airworthiness Division, FAA, 3960 Paramount Blvd., Lakewood, CA 90712; phone 562-627-5251; email [email protected]. \n\n\n\tIssued on August 21, 2020. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. (FR Doc. 2020-18829 Filed 8-26-20; 8:45 am) BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2024-10-292024-05 · Engine/Transmission Coupling, Gearmotor Assembly
2022-11-212022-21 · EMERGENCY FLOTATION SECTION, Pop-Out Float Under-inflation.
2022-04-11AIR-22-08 · MAIN ROTOR DRIVE SYSTEM,TAIL ROTOR DRIVE SYSTEM
2022-03-03AIR-22-03 · Robinson Helicopter Company Model R22, R44, and R66 Helicopters; Emergency Locator Transmitter Retention
2021-08-24AIR-21-14 · Robinson R44 and R66 HeliSAS Autopilot/Garmin Primary Flight Display (PFD) Interface

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 30, 2026. Connections as data: /graph/directive/2020-18-08.json · aircraft systems.